A power flow mode method based on the imaginary part of the dynamic flexibility matrix is presented, which allows determining eigenvalues and eigenvectors representing qualitative and quantitative information on the power flowing inside the structure, respectively.
Then, for the key technologies of aero-engines switching control, a design algorithm is presented which can determine which candidate controller should be put in feedback with the plant to achieve a desired performance and the procedure to design the aircraft engine multi-loop control system is detailed.
A generalized derivation is presented which not only determines necessary and sufficient conditions for the application of this approximate description, but also gives estimates for its errors.
A GCPM design approach based on stationary phase approximation is presented which helps to determine the initial parameter of phase mask, significantly decreasing the computational time required for numerical simulation.
A methodology is presented which allows to determine the coefficients of transmission and reflection of plane acoustic waves at flow discontinuities in piping systems by combining large eddy simulation (LES) of turbulent compressible flows with system identification.
In this section, simple empirical equations are presented which are used for determining geometrical properties of free-electron metal nanostructures.
Various quantitative measures for the assessment of potency are also presented, which could assist in determining how to handle substances in the risk assessment when a regulatory concern is identified.
Now we are ready to present a formula which determines the coefficients (a_{j}) in (2.2) with the help of the partition function given by the following lemma.
In this study an analytical numerical method is presented which can be used to determine the dynamic response of beams carrying a moving mass, with various boundary conditions.
